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Rotary extending-retracting mechanism of exposed device of aircraft

A technology of retractable mechanism and equipment, which is applied in the direction of aircraft parts, transportation and packaging, etc., can solve the problems affecting the structural layout of the aircraft and the high longitudinal space requirements of the aircraft, and achieve the effects of light weight, reliable fixation and stable transmission

Active Publication Date: 2014-03-19
JIANGXI HONGDU AVIATION IND GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The conventional retractable mechanism is in the form of vertical retraction, which has high requirements for the longitudinal space of the aircraft and affects the structural layout of the aircraft.

Method used

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  • Rotary extending-retracting mechanism of exposed device of aircraft
  • Rotary extending-retracting mechanism of exposed device of aircraft
  • Rotary extending-retracting mechanism of exposed device of aircraft

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Experimental program
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Embodiment Construction

[0017] Attached below figure 1 , 2 , 3, 4, 5, 6 describe the present invention in detail:

[0018] A rotating retractable mechanism for aircraft exposed equipment, the mechanism includes an equipment cabin door frame 1, a rocker arm 2, a mouth frame connection structure 3, an adjustable connecting rod 4, a contact switch 5, a driving rocker arm 6, and an equipment cabin structure wall panel 7. Connecting bolt 8, driving shaft 9, follower base 10, equipment base 11, exposed equipment 12, equipment rotating shaft 13, limit structure 14;

[0019] The equipment cabin structural wall 7 and the equipment cabin door frame 1 are fixedly connected through the mouth frame connecting structure 3 to form an equipment cabin for installing equipment, and are connected to the aircraft structure on the structural wall through connecting bolts 8 . In order to realize the function of releasing the exposed equipment 12 out of the cabin and entering the designated position in the cabin, su...

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PUM

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Abstract

The invention relates to a rotary extending-retracting mechanism of an exposed device of an aircraft and belongs to the technical field of aircraft manufacturing. The rotary extending-retracting mechanism comprises a device cabin doorway frame, a rocker arm, a doorway frame connecting structure, an adjustable connecting rod, a contact switch, a driving rocker arm, a device cabin structure wall board, a connecting bolt, a driving rotation shaft, a following-up base, a device base, the exposed device, a device rotation shaft and a limiting structure. The rotary extending-retracting mechanism can achieve a rotary extending-retracting function of the device on the aircraft, has the advantages of being stable in transmission, reliable in fixing, light in weight and the like, is a novel rotary extending-retracting mechanism for the extending device required to be shortened by the aircraft and effectively utilizes a limited installing space of the aircraft.

Description

technical field [0001] The invention relates to a rotary retractable mechanism for aircraft exposed equipment, which belongs to the technical field of aircraft manufacturing. Background technique [0002] Usually, in order to complete specific tasks, the aircraft needs to load some equipment that protrudes from the surface of the aircraft, such as optoelectronic platform equipment, large antennas, etc. Some of these equipment are only used for a short period of time in a certain period of time. If they are directly installed on the surface of the aircraft, they will Affect the aerodynamic and stealth performance of the aircraft. The retractable design of such equipment can effectively improve the aerodynamic and stealth performance of the aircraft. [0003] The conventional retractable mechanism is in the form of vertical retraction, which requires higher longitudinal space of the aircraft and affects the structural arrangement of the aircraft. SUMMARY OF THE INVENTION ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D47/00
Inventor 辛荣提沈亮冷智辉刘敏符松海何明清
Owner JIANGXI HONGDU AVIATION IND GRP